CN205231625U - Unmanned aerial vehicle laser removes barrier device - Google Patents

Unmanned aerial vehicle laser removes barrier device Download PDF

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Publication number
CN205231625U
CN205231625U CN201521022932.2U CN201521022932U CN205231625U CN 205231625 U CN205231625 U CN 205231625U CN 201521022932 U CN201521022932 U CN 201521022932U CN 205231625 U CN205231625 U CN 205231625U
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CN
China
Prior art keywords
laser
support
unmanned plane
detector
arranges
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Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201521022932.2U
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Chinese (zh)
Inventor
牟善峰
孙士年
刘加峰
于宏志
尹国慧
李修金
陈育淦
纽文彬
吴善船
许光明
徐勤法
许崇友
王建金
张怀宗
相起业
王鹏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
State Grid Corp of China SGCC
Maintenance Branch of State Grid Shandong Electric Power Co Ltd
Original Assignee
State Grid Corp of China SGCC
Maintenance Branch of State Grid Shandong Electric Power Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by State Grid Corp of China SGCC, Maintenance Branch of State Grid Shandong Electric Power Co Ltd filed Critical State Grid Corp of China SGCC
Priority to CN201521022932.2U priority Critical patent/CN205231625U/en
Application granted granted Critical
Publication of CN205231625U publication Critical patent/CN205231625U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

Unmanned aerial vehicle laser removes barrier device, including the unmanned aerial vehicle body, the lower part installing support of unmanned aerial vehicle body, the lower part installation laser power of support with the jar sprays paint, a side -mounting shower nozzle and a laser emitter of support, laser power passes through the wire and connects laser emitter, the delivery outlet installation hose that sprays paint jar, the one end connection nozzle of hose. The utility model discloses a shower nozzle coats with lacquer with jar black that spouts on the surface to shallow colour or transparent " barrier " that sprays paint, increases the effect that stops to the light beam, reduces the transmission, increase cutting energy. The utility model discloses can spout into black with transparent film before laser cutting, and then use laser emitter release laser to cut the operation to can make that unmanned aerial vehicle laser removes barrier device can to shallow colour or transparent " barrier " cuts.

Description

Unmanned plane laser failure eliminating device
Technical field
The present invention relates to a kind of laser failure eliminating device, specifically a kind of unmanned plane laser failure eliminating device.
Background technology
Along with the continuous progress of science and technology, unmanned plane gradually apply to power industry, and carry motion arm to alive circuit by unmanned plane and carry out defect expressivity, progressively become the trend of electric power development.Removing the foreign matter that power line conductive, ground wire hang is an important process, the serious consequence such as line short, tripping operation is likely caused as processed not in time, the laser that existing unmanned plane laser failure eliminating device sends is for transparent plastic film, laser beam can through plastic film, most energy cannot be gathered on film, so cannot realize cutting; And for opaque light colour object, laser beam then major part can be reflected, cutting also cannot be realized.
Summary of the invention
The object of this invention is to provide a kind of unmanned plane laser failure eliminating device, can solve the problem.
The present invention for achieving the above object, be achieved through the following technical solutions: unmanned plane laser failure eliminating device, comprise unmanned plane body, the lower mounting bracket of unmanned plane body, Laser Power Devices and spray paint can are installed, the side mounting spray head of support and generating laser in the bottom of support, and Laser Power Devices connect generating laser by wire, the delivery outlet of spray paint can installs flexible pipe, and one end of flexible pipe connects shower nozzle.
In order to realize object of the present invention further, can also by the following technical solutions: the present invention also comprises transformer main frame and detector, support bar is installed in the both sides, bottom of described support, support bar is arranged electric push rod and sleeve, the piston rod of electricity push rod coordinates with sleeve, the end attachment plug of sleeve, plug is arranged on the bottom of support bar, transformer main frame is provided with oil drum, detector comprises detector housing, inside arrange spectrometer unit and device for filtering impurities, device for filtering impurities comprises support, and support installs two volume measuring instruments and filter, two volume measuring instruments are arranged on the upper and lower of filter respectively, volume measuring instrument and positioned inline, volume measuring instrument is made up of bottle, separation net, infrared survey instrument and floater shot, bottle upper and lower arranges import and outlet respectively, and arrange vertical separation net in bottle, floater shot is positioned at bottle, bottle upper side installation infrared measuring instrument, infrared survey instrument is positioned at floater shot side, filter is made up of filtration barrel body, several screen pack and upper cover, and filtration barrel body inwall arranges fixture block, and several screen pack distributes up and down, is coordinated each other by support bar, and support bar card is placed on fixture block, and upper cover coordinates with filtration barrel body, upper cover is connected by flexible pipe with the volume measuring instrument on filter top, arranged for the second communicating pipe between device for filtering impurities and spectrometer unit, the second communicating pipe was provided with delivery pump, the oil drum of transformer main frame arranges thief hole, detector housing is arranged style connecting hole, style connecting hole connects import, plug can coordinate with thief hole or style connecting hole respectively, several rubber blanket is installed in the bottom of described support, the oil drum of transformer main frame is arranged several transformer mating holes, detector housing is arranged several detector mating holes, rubber blanket can coordinate with transformer mating holes and detector mating holes, between described spectrometer unit and device for filtering impurities, de-watering apparatus is set, third connecting pipe is set between de-watering apparatus and spectrometer unit, second communicating pipe arranged triple valve, triple valve connects one end of the first communicating pipe, the other end of the first communicating pipe connects de-watering apparatus, de-watering apparatus comprises base, and base installs two weighers and vacuum drainage cylinder, and two weighers lay respectively at vacuum drainage cylinder two ends, and weigher is connected with vacuum drainage cylinder, weigher is made up of weighing cup and electronic scale, and weighing cup is fixedly mounted on the top of electronic scale, vacuum drainage cylinder comprises cylindrical shell, arranges heating rod in cylindrical shell, and the top of cylindrical shell arranges gas-liquid separator, and gas-liquid separator connects vacuum pump.Described spectrometer unit is arranged input keyboard, input keyboard and display screen, display screen is connected with spectrometer unit by input keyboard.Detector housing outside is exposed at outside the display screen of described spectrometer unit.
The invention has the advantages that: the present invention sprays black paint by shower nozzle and spray paint can on light colour or the surface of transparent " barrier ", increase the barrier effect to light beam, reduce transmission, increase ablation energy, transparent membrane can be sprayed into black by the present invention before laser cutting, and then use generating laser release laser to carry out cutting operation, thus unmanned plane laser failure eliminating device can be made can to cut light colour or transparent " barrier ", the present invention also has advantage compact, cheap for manufacturing cost and easy to use simple for structure.
Accompanying drawing explanation
Fig. 1 is one of structural representation of the present invention; Fig. 2 is structural representation two of the present utility model; Fig. 3 is detector arrangement schematic diagram; Fig. 4 is the I partial enlargement structural representation of Fig. 3; Fig. 5 is the II partial enlargement structural representation of Fig. 3; Fig. 6 is the III partial enlargement structural representation of Fig. 2; Fig. 7 is the IV partial enlargement structural representation of Fig. 3; Fig. 8 is structural representation three of the present utility model.
Reference numeral: 1 support bar 2 rubber blanket 3 unmanned plane body 4 shower nozzle 5 generating laser 6 Laser Power Devices 7 flexible pipe 8 spray paint can 9 support 10 weigher 11 triple valve 12 delivery pump 13 support 14 volume measuring instrument 15 filter 16 first communicating pipe 17 second communicating pipe 18 vacuum pump 19 gas-liquid separator 20 third connecting pipe 21 bottle 22 separation net 23 infrared survey instrument 24 floater shot 25 import 26 exports 27 filtration barrel body 28 fixture block 29 screen pack 30 support bar 31 upper cover 32 detector housing 33 electric push rod 34 sleeve 35 plug 36 thief hole 37 oil drum 38 transformer body 39 transformer mating holes 40 detector mating holes 41 style connecting hole 42 spectrometer unit 43 input keyboard 44 overturning seat 45 display screen 46 weighing cup 47 electronic scale 48 vacuum drainage cylinder 49 base 50 heating rod.
Embodiment
Unmanned plane laser failure eliminating device, as shown in the figure, comprise unmanned plane body 3, the lower mounting bracket 9 of unmanned plane body 3, Laser Power Devices 6 and spray paint can 8 are installed, the side mounting spray head 4 of support 9 and generating laser 5 in the bottom of support 9, and Laser Power Devices 6 connect generating laser 5 by wire, the delivery outlet of spray paint can 8 installs flexible pipe 7, and one end of flexible pipe 7 connects shower nozzle 4.
The present invention sprays black paint by shower nozzle 4 and spray paint can 8 on light colour or the surface of transparent " barrier ", increase the barrier effect to light beam, reduce transmission, increase ablation energy, transparent membrane can be sprayed into black by the present invention before laser cutting, and then use generating laser 5 to discharge laser to carry out cutting operation, thus unmanned plane laser failure eliminating device can be made can to cut light colour or transparent " barrier ".
In current electric power system, transformer main frame hanging position is higher, there are insoluble greasy filth, fiber and foul etc. in the transformer oil of the Long-Time Service in transformer, these materials may cause spectrometer to block, cause fault together, in order to overcome the problems referred to above, the present invention also comprises transformer main frame 38 and detector, described support 9) both sides, bottom install support bar 1, support bar 1 is arranged electric push rod 33 and sleeve 34, the piston rod of electricity push rod 33 coordinates with sleeve 34, the end attachment plug 35 of sleeve 34, and plug 35 is arranged on the bottom of support bar 1, transformer main frame 38 is provided with oil drum 37, detector comprises detector housing 32, spectrometer unit 42 and device for filtering impurities are inside set, device for filtering impurities comprises support 13, support 13 installs two volume measuring instruments 14 and filter 15, two volume measuring instruments 14 are arranged on the upper and lower of filter 15 respectively, and volume measuring instrument 14 and filter 15 are connected, volume measuring instrument 14 is made up of bottle 21, separation net 22, infrared survey instrument 23 and floater shot 24, bottle 21 upper and lower arranges import 25 and outlet 26 respectively, vertical separation net 22 is set in bottle 21, floater shot 24 is positioned at bottle 21, bottle 21 upper side installation infrared measuring instrument 23, infrared survey instrument 23 is positioned at floater shot 24 side, filter 15 is made up of filtration barrel body 27, several screen pack 29 and upper cover 31, filtration barrel body 27 inwall arranges fixture block 28, and several screen pack about 29 distributes, and is coordinated each other by support bar 30, support bar 30 card is placed on fixture block 28, and upper cover 31 coordinates with filtration barrel body 27, upper cover 31 is connected by flexible pipe with the volume measuring instrument 14 on filter 15 top, arrange between device for filtering impurities and spectrometer unit 42 and be provided with delivery pump 12 second communicating pipe 17 communicating pipe 17, second, the oil drum 37 of transformer main frame 38 arranges thief hole 36, detector housing 32 is arranged style connecting hole 41, style connecting hole 41 connects import 25, plug 35 can coordinate with thief hole 36 or style connecting hole 41 respectively, transformer oil can carry out timing and detect, avoid because the normal operation of oil quality variable effect transformer, the present invention is connect by nobody and samples transformer oil easily, during sampling, plug 35 is inserted in thief hole 36, is pulled by electric push rod 33 and make sleeve 34 produce negative pressure, thus complete sampling, by unmanned plane, sample oil is transported to detector place, plug 35 is inserted into style connecting hole 41, electricity push rod 33 promotes to make to detect in the oil of the sample in sleeve 34 Injection Detector, tested transformer oil can be filtered before detection, by insoluble greasy filth, fiber and dirt filtration are out, spectrometer is avoided to block, after being filtered by device for filtering impurities, the volume number obtained shared by impurity can be calculated, determine tested transformer oil reuses after whether can carrying out filtration treatment, thus determine whether to be necessary the transformer oil that again renews, avoid waste, clear up after filtration conveniently.Transformer oil after filtration, after kaleidophon detects, can reduce the impact of solid matter, discharges physical factor, obtains experimental result and more press close to production and application.
In order to improve the accuracy of cooperation, several rubber blanket 2 is installed in the bottom of described support 9, the oil drum 37 of transformer main frame 38 arranges several transformer mating holes 39, detector housing 32 is arranged several detector mating holes 40, rubber blanket 2 can coordinate with transformer mating holes 39 and detector mating holes 40, soft rubber blanket 2 can prevent support 9 and ground rigid contact, support 9 is avoided to damage, after rubber blanket 2 coordinates with transformer mating holes 39 or detector mating holes 40, precision during sampling can be improved.
Owing to also there is a lot of moisture in transformer oil, moisture also can affect testing result, detecting the water content of the transformer oil of Long-Time Service is also an important indicator, in order to realize lab scale test, between described spectrometer unit 42 and device for filtering impurities, de-watering apparatus is set, third connecting pipe 20 is set between de-watering apparatus and spectrometer unit 42, second communicating pipe 17 arranged triple valve 11, triple valve 11 connects one end of the first communicating pipe 16, and the other end of the first communicating pipe 16 connects de-watering apparatus, de-watering apparatus comprises base 8, and on base 8, installation two weighers 10 and vacuum drainage cylinder 48, two weighers 10 lay respectively at vacuum drainage cylinder 48 two ends, and weigher 10 is connected with vacuum drainage cylinder, weigher 10 is made up of weighing cup 46 and electronic scale 47, and weighing cup 46 is fixedly mounted on the top of electronic scale 47, vacuum drainage cylinder 48 comprises cylindrical shell, heating rod 50 is set in cylindrical shell, the top of cylindrical shell arranges gas-liquid separator 19, gas-liquid separator 19 connects vacuum pump 18, transformer oil after filtration is added in weigher 10 and weighs, enter in vacuum drainage cylinder 48 after weighing, improving temperature by heating rod 50 is moisture evaporation, pressure is reduced by vacuum pump 18, moisture in transformer oil is extruded, moisture is separated through gas-liquid separator 19, transformer oil after draining weighs entering another weigher 10, thus determine the water content in transformer oil, can judge whether transformer oil can be recycled according to water content.
Described spectrometer unit 42 is arranged input keyboard 43, input keyboard 44 and display screen 45; display screen 45 is connected with spectrometer unit 42 by input keyboard 44; display screen 45 and input keyboard 43 are structure as a whole with spectrometer main frame 1; easy to use; without the need to other connection device; when not using, display screen 45 turnover can be protected display screen 45; display screen 45 can cover on input keyboard 43; also input keyboard 43 can be protected; detector housing 32 is exposed at outside, convenient observation and process outside the display screen 45 of described spectrometer unit 42.
Technical scheme of the present invention is not restricted in the scope of embodiment of the present invention, and the technology contents of the not detailed description of the present invention is known technology.

Claims (6)

1. unmanned plane laser failure eliminating device, it is characterized in that: comprise unmanned plane body (3), the lower mounting bracket (9) of unmanned plane body (3), Laser Power Devices (6) and spray paint can (8) are installed in the bottom of support (9), the side mounting spray head (4) of support (9) and generating laser (5), Laser Power Devices (6) connect generating laser (5) by wire, and the delivery outlet of spray paint can (8) installs flexible pipe (7), and one end of flexible pipe (7) connects shower nozzle (4).
2. unmanned plane laser failure eliminating device according to claim 1, it is characterized in that: also comprise transformer main frame (38) and detector, support bar (1) is installed in the both sides, bottom of described support (9), support bar (1) is arranged electric push rod (33) and sleeve (34), the piston rod of electricity push rod (33) coordinates with sleeve (34), the end attachment plug (35) of sleeve (34), plug (35) is arranged on the bottom of support bar (1); Transformer main frame (38) is provided with oil drum (37); Detector comprises detector housing (32), spectrometer unit (42) and device for filtering impurities are inside set, device for filtering impurities comprises support (13), upper installation two volume measuring instruments (14) of support (13) and filter (15), two volume measuring instruments (14) are arranged on the upper and lower of filter (15) respectively, volume measuring instrument (14) and filter (15) series connection; Volume measuring instrument (14) is made up of bottle (21), separation net (22), infrared survey instrument (23) and floater shot (24), bottle (21) upper and lower arranges import (25) and outlet (26) respectively, vertical separation net (22) is set in bottle (21), floater shot (24) is positioned at bottle (21), bottle (21) upper side installation infrared measuring instrument (23), infrared survey instrument (23) is positioned at floater shot (24) side; Filter (15) is made up of filtration barrel body (27), several screen pack (29) and upper cover (31), filtration barrel body (27) inwall arranges fixture block (28), several screen pack (29) distributes up and down, coordinated by support bar (30) each other, support bar (30) card is placed on fixture block (28), and upper cover (31) coordinates with filtration barrel body (27); Upper cover (31) is connected by flexible pipe with the volume measuring instrument (14) on filter (15) top; Arrange the second communicating pipe (17) between device for filtering impurities and spectrometer unit (42), the second communicating pipe (17) is provided with delivery pump (12); The oil drum (37) of transformer main frame (38) arranges thief hole (36), detector housing (32) is arranged style connecting hole (41), style connecting hole (41) connects import (25); Plug (35) can coordinate with thief hole (36) or style connecting hole (41) respectively.
3. unmanned plane laser failure eliminating device according to claim 2, it is characterized in that: several rubber blanket (2) is installed in the bottom of described support (9), the oil drum (37) of transformer main frame (38) arranges several transformer mating holes (39), detector housing (32) is arranged several detector mating holes (40), rubber blanket (2) can coordinate with transformer mating holes (39) and detector mating holes (40).
4. unmanned plane laser failure eliminating device according to claim 2, it is characterized in that: between described spectrometer unit (42) and device for filtering impurities, de-watering apparatus is set, third connecting pipe (20) is set between de-watering apparatus and spectrometer unit (42), arranged triple valve (11) second communicating pipe (17), triple valve (11) connects one end of the first communicating pipe (16), and the other end of the first communicating pipe (16) connects de-watering apparatus; De-watering apparatus comprises base (8), upper installation two weighers (10) of base (8) and vacuum drainage cylinder (48), and two weighers (10) lay respectively at vacuum drainage cylinder (48) two ends, and weigher (10) is connected with vacuum drainage cylinder; Weigher (10) is made up of weighing cup (46) and electronic scale (47), and weighing cup (46) is fixedly mounted on the top of electronic scale (47); Vacuum drainage cylinder (48) comprises cylindrical shell, arranges heating rod (50) in cylindrical shell, and the top of cylindrical shell arranges gas-liquid separator (19), and gas-liquid separator (19) connects vacuum pump (18).
5. unmanned plane laser failure eliminating device according to claim 2, it is characterized in that: described spectrometer unit (42) is arranged input keyboard (43), input keyboard (44) and display screen (45), display screen (45) is connected with spectrometer unit (42) by input keyboard (44).
6. unmanned plane laser failure eliminating device according to claim 5, is characterized in that: be exposed at detector housing (32) outside the display screen (45) of described spectrometer unit (42) outside.
CN201521022932.2U 2015-12-10 2015-12-10 Unmanned aerial vehicle laser removes barrier device Expired - Fee Related CN205231625U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521022932.2U CN205231625U (en) 2015-12-10 2015-12-10 Unmanned aerial vehicle laser removes barrier device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521022932.2U CN205231625U (en) 2015-12-10 2015-12-10 Unmanned aerial vehicle laser removes barrier device

Publications (1)

Publication Number Publication Date
CN205231625U true CN205231625U (en) 2016-05-11

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105337220A (en) * 2015-12-10 2016-02-17 国家电网公司 Unmanned aerial vehicle laser cutting barrier removing device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105337220A (en) * 2015-12-10 2016-02-17 国家电网公司 Unmanned aerial vehicle laser cutting barrier removing device

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C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160511

Termination date: 20161210

CF01 Termination of patent right due to non-payment of annual fee